J Class Rocket Motor

AeroTech J1799N

Name: AeroTech J1799N Rocket Motor
Creator: Veenie Aerospace
License: https://creativecommons.org/licenses/by/4.0/

AeroTech

Warp 9

Ø 54mm

Total Impulse

1214.8Ns

Burn Time

0.61s

Avg Thrust

1963.4N

Max Thrust

2965.9N

Thrust Profile (N)

0.61s Burn Window

Engineered by AeroTech, the J1799N is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1214.8 Ns over a 0.61 second burn window.

With an average thrust of 1963.4 N and a peak of 2965.9 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Warp 9 propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.

Diameter 54 mm

Length 330 mm

Hardware RMS-54/1280

Delays (s) P

Specific Impulse 209.5 s

Peak Thrust 2114.01 N

Peak Time T+ 0.144s

T/W Ratio 180.15

Propellant Warp 9

Profile dual-peak

Type reload

Sparky No

Mass Budget

1111g Total

Casing (Dry)

520.0g

46.8%

Propellant

591.0g

53.2%

Live Sizing

Flight Envelope

Body Diameter 38 mm

Motor Mount 29 mm

Dry Mass 500 g

Target Apogee 1000 m

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